Failure Criterion‐Based Bead Optimization of a Wind Turbine Blade Root Section
ABSTRACT This study presents a bead‐based optimization framework for fiber composite wind turbine blades, employing the Tsai–Wu failure criterion as the structural performance measure. The objective is to design an optimal transition geometry between an existing blade and a root section with 20% smaller diameter, while preserving the original material ...
Philipp Ulrich Haselbach +4 more
wiley +1 more source
Data-driven aerodynamic shape optimization of rotor airfoils based on deep learning
As the fundamental component of rotor blades, the airfoil dominates the aerodynamic performance of helicopter rotors. The aerodynamic shape optimization of rotor airfoils is thus an effective means of improving their aerodynamic performance.
Jiaqi Liu +3 more
doaj +1 more source
Aerodynamic Sensitivity Analysis for a Wind Turbine Airfoil in an Air-Particle Two-Phase Flow
In this paper, the Navier-Stokes equations coupled with a Lagrangian discrete phase model are described to simulate the air-particle flows over the S809 airfoil of the Phase VI blade, the NH6MW25 airfoil of a 6 MW wind turbine blade and the NACA0012 ...
Tongqing Guo +4 more
doaj +1 more source
Wind tunnel experiments were conducted on a 2-blade horizontal axis wind rotor to investigate the effect of pitch angle and Reynolds number on aerodynamic characteristics.
J. Y. Zhu, P. Q. Liu
doaj
BOUNDARY LAYER AND AMPLIFIED GRID EFFECTS ON AERODYNAMIC PERFORMANCES OF S809 AIRFOIL FOR HORIZONTAL AXIS WIND TURBINE (HAWT) [PDF]
The design of rotor blades has a great effect on the aerodynamics performances of horizontal axis wind turbine and its efficiency. This work presents the effects of mesh refinement and boundary layer on aerodynamic performances of wind turbine S809 rotor.
YOUNES EL KHCHINE, MOHAMMED SRITI
doaj
Effect of Airfoil Concavity on Wind Turbine Blade Performances
Although the optimization of wind turbine blade aerodynamic performance has achieved fruitful results, whether airfoil concavity, an important method for preventing flow separation, is also feasible for improving the aerodynamic performance has not been ...
Jianlong Ma +6 more
doaj +1 more source
Study Of The Aerodynamic Structure Around A NACA6409 Airfoil Rotor
The multi-copters are one of the important aircrafts in the world because they are used in both military and civil application. The problem of these aircrafts is the low efficiency of its propellers. That’s why, it is necessary to study the aerodynamic structure around every rotor.
openaire +3 more sources
Turbine Airfoil Leading Edge Film Cooling Bibliography: 1972–1998
Film cooling for turbine airfoil leading edges has been a common practice for at least 35 years as turbine inlet gas temperatures and pressures have continually increased along with cooling air temperatures for higher engine cycle efficiency.
D. M. Kercher
doaj +1 more source
Aerodynamic performance and wake development of NACA 0018 airfoil with serrated gurney flaps
Improving the aerodynamic performance of the airfoil is important for optimising the rotor efficiency of the vertical axis wind turbines. As a simple passive control method, the Gurney flap is widely used to improve the aerodynamic performance of ...
Zhehui Zheng, Liu Chen
doaj +1 more source
Dynamic stall characteristics of a rotor airfoil under coupled pitching-plunging motions
The blade of a helicopter rotor encounters plunging motion in addition to periodic pitching oscillations during actual flight, which complicates the flow field structure and dynamic stall characteristics.
Jiaqiang WU +5 more
doaj +1 more source

